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Aircraft landing port and aircraft landing method

机译:飞机降落港及飞机降落方法

摘要

PROBLEM TO BE SOLVED: To easily and surely land an air vehicle at a fixed position. A landing port of an aircraft having a pedestal portion and a plurality of legs extending below the pedestal portion, wherein the plurality of legs of the aircraft descending from above contact each other. It has a conical surface that can be formed. The landing port has a truncated cone-shaped portion, the cone surface is the cone surface of the portion, and the portion near the top surface of the truncated cone-shaped portion is surrounded by the pedestal portion and the plurality of legs. The shape fits in space. The air vehicle has a power receiving coil near the pedestal part of the space for receiving power by non-contact power feeding, and the landing port supplies power to the power receiving coil near the top surface of the truncated cone. Equipped with a power transmission coil. The power transmission coil is provided so that the power transmission surface faces the power receiving surface of the power receiving coil in a state where the space is accommodated in a portion near the top surface of the truncated cone shape portion. [Selection diagram] Fig. 1B
机译:要解决的问题:轻松可靠地将飞机降落在固定位置。飞机的着陆端口,其具有基座部分和在基座部分下方延伸的多个支腿,其中,飞机的多个支腿从上方下降。它具有可以形成的圆锥形表面。着陆口具有截头圆锥形部分,圆锥表面是该部分的圆锥表面,并且截头圆锥形部分的顶表面附近的部分被基座部分和多个支腿围绕。形状适合空间。该飞行器在空间的基座部分附近具有电力接收线圈,用于通过非接触电力馈送来接收电力,并且着陆端口向截锥的顶表面附近的电力接收线圈供电。配有输电线圈。设置送电线圈,使得在截锥形状部分的顶表面附近的部分中容纳有空间的状态下,送电表面面向受电线圈的受电表面。 [选择图]图1B

著录项

  • 公开/公告号JP2020125044A

    专利类型

  • 公开/公告日2020-08-20

    原文格式PDF

  • 申请/专利权人 中国電力株式会社;

    申请/专利号JP20190019041

  • 发明设计人 沖原 潤;谷川 博昭;大久保 典浩;

    申请日2019-02-05

  • 分类号B64F1/12;B64C27/08;B64D27/24;B64C25/06;B64F1/28;

  • 国家 JP

  • 入库时间 2022-08-21 11:37:45

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